INSTALLATION OF HARNESS ASSEMBLIES (ELECTRICAL WIRING), SPACE VEHICLE, GENERAL SPECIFICATION FOR

Published date

01-01-2009

Publisher

National Aeronautics and Space Administration

1 SCOPE
2 APPLICABLE DOCUMENTS
3 REQUIREMENTS
4 QUALITY ASSURANCE
5 NOTES
6 DEFINITIONS
7 ACRONYMS AND ABBREVIATIONS

Defines requirements for the design of installation and the actual installation of electrical harness assemblies in space vehicles and payloads.

DocumentType	Standard
PublisherName	National Aeronautics and Space Administration
Status	Current

NASA MSFC SPEC 250 : 1963	PROTECTIVE FINISHES FOR SPACE VEHICLE STRUCTURES AND ASSOCIATED FLIGHT EQUIPMENT GENERAL SPECIFICATION FOR
NASA STD 8739.1 : 2016	WORKMANSHIP STANDARD FOR POLYMERIC APPLICATION ON ELECTRONIC ASSEMBLIES
NASA STD 6001 : 2011	FLAMMABILITY, OFFGASSING, AND COMPATIBILITY REQUIREMENTS AND TEST PROCEDURES
NASA STD 4003 : 2013	ELECTRICAL BONDING FOR NASA LAUNCH VEHICLES, SPACECRAFT, PAYLOADS, AND FLIGHT EQUIPMENT
MIL-STD-889 Revision C:2016	DISSIMILAR METALS
ESD S20.20 : 2014	PROTECTION OF ELECTRICAL AND ELECTRONIC PARTS, ASSEMBLIES AND EQUIPMENT (EXCLUDING ELECTRICALLY INITIATED EXPLOSIVE DEVICES)
NASA STD 8739.4 : 2016	WORKMANSHIP STANDARD FOR CRIMPING, INTERCONNECTING CABLES, HARNESSES, AND WIRING
MIL-STD-1576 Base Document:1984	ELECTROEXPLOSIVE SUBSYSTEM SAFETY REQUIREMENTS AND TEST METHODS FOR SPACE SYSTEMS
NASA STD 3000 VOL 1 : 1995	MAN-SYSTEMS INTEGRATION STANDARDS - VOLUME 1

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NASA MSFC SPEC 494 : 2009